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RISThe Influence of Inlet Fogging for the Stable Range in a Transonic Compressor Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The inlet fogging effects on the stable range of a NASA transonic compressor stage, Stage 35, are numerically simulated and analyzed in this paper. The 3D two-phase flow fields in the compressor ...
The Effects of Wet Compression and Blade Tip Water Injection on the Stability of a Transonic Compressor Rotor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The rotor blade tip leakage flow and associated formation of the tip leakage vortex and interaction of the tip leakage vortex with the shockwave, particularly in the case of a transonic ...